Integrated guide vane assembly

Details Integrated guide vane assembly Integrated guide vane assembly

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01)

Patent

CA 2680629

An integrated outlet guide vane assembly for turbomachinery typically includes at least one outlet guide vane (70) and at least one bifurcation (80) having a leading edge and a trailing edge. The turbomachinery has a central axis of rotation (11) and a defined direction of rotation (D) about the axis (11). The guide vane (70) comprises an airfoil having a leading edge (71) and a trailing edge (73) and has a non- zero angle of lean (L) in the direction of rotation (D) and a non-zero sweep angle (S) relative to a line perpendicular to the central axis (11). The leading edge of the bifurcation (80) has a non-zero angle of lean (L) in the direction of rotation (D) and a non-zero sweep angle (S) relative to a line perpendicular to the central axis (11). The trailing edge (73) of the vane (70) is faired into the leading edge of the bifurcation (80).

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